Resolvent-based control of streaks in boundary layers
2018 (English)In: 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018, International Council of the Aeronautical Sciences , 2018Conference paper, Published paper (Refereed)
Abstract [en]
In the present work, we investigate efficient placement of sensors and actuators for closed-loop control of boundary-layer flows. The focus of this work is on the transitional flow cases where perturbation field is dominated by streaks. This is done using a reduced-order model based on resolvent analysis, an approach that also allows us to analyse the sensitivity of the flow response to control. A numerical sensitivity analysis was performed in this first approach, leading to conclusions about best choices of velocity components to be sensed and directions to be forced. Afterwards, we compared the performance between gaussian and shear sensors at the wall, focusing on the damping of the first resolvent gain using these devices. We close the work with the analysis of a plasma actuator, a configuration closer to standard choices for this kind of problem in both simulations and experiments.
Place, publisher, year, edition, pages
International Council of the Aeronautical Sciences , 2018.
Keywords [en]
Control, Transition, Turbulence, Actuators, Boundary layer flow, Control engineering, Sensitivity analysis, Closed-loop control, Numerical sensitivity, Placement of sensors, Plasma actuator, Reduced order models, Transitional flow, Velocity components, Boundary layers
National Category
Fluid Mechanics
Identifiers
URN: urn:nbn:se:kth:diva-247423Scopus ID: 2-s2.0-85060461608ISBN: 9783932182884 (print)OAI: oai:DiVA.org:kth-247423DiVA, id: diva2:1305798
Conference
31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018, 9 September 2018 through 14 September 2018
Note
QC20190418
2019-04-182019-04-182025-02-09Bibliographically approved